Commonwealth legislation

AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

1/10 complexity

This AD mandates inspection of the retaining bolt on the main landing‑gear torque‑link pin for specified Twin Commander (Gulfstream/Rockwell/Aerocommander) models/serial ranges to prevent the torque‑link pin from working loose and compromising the landing gear. Affected aircraft must be inspected within 25 flight hours after 22 August 1978 using the procedure in Rockwell Service Letter No. 319.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection.

AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue 9/1978,Aircraft below 5700 kg,Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes,Main Landing Gear Torque Link Pin Retaining Bolt - Inspection,69 title: Airworthiness Directive - AD/AC/69 - Main Landing Gear Torque Link Pin Retaining Bolt - Inspection

?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

AD/AC/69 Main Landing Gear Torque Link Pin Retaining Bolt - Inspection

9/78

Applicability: All models 500A, 500B, 500U, 500S, 560F, 680F(P), 680FL, 680FL(P), 680T, 680V

and 680W with S/Nos. 871 to 1876, and Model 500S with S/Nos. 3050 and subsequent; All model 681 with S/Nos. 6001 to 6072;

All model 685 with S/Nos. 1200 to 12066;

All models 690, 690A and 690B with S/Nos. 11001 and subsequent.

Document: Rockwell International SL No. 319.

Compliance: Within 25 hours’ time in service after 22 August 1978.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.